Spidertracks Spider 3, Инструкция по эксплуатации

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(B)Spider 6 Structure Test Procedure
(B)1.Test Definition
The purpose of these test procedures is to demonstrate structural integrity for the installation
of the Spider 6.
(B)2.Special Tools and Equipment
A calibrated digital or analogue fish hook type scale (e.g. Transducer Techniques HFG-110)
is required to conduct the structural testing.
(B)3.Test Conditions
The Spider 6 must be installed prior to starting the structural testing. Allow for adequate time
for the adhesive to fully bond to the installation location.
(B)4.Applied Loads
Conservative ultimate load factors for structural testing purposes are provided for FAR 23
(normal, acrobatic and utility category airplanes) and FAR 27 (normal rotorcraft)
installations. For additional information, refer to the acceptable data source, FAA
AC43.13-2B, Chapter 1, Paragraphs 103 through 105.
Table 1: Minimum Applied Loads.
(B)5.Test Procedure
The following procedures detail the methodology for the structural test.
1. Record the serial number of the Spider 6 being used in the test and complete the test
record information.
2. Apply the minimum loads listed in Chapter 3.4 to the centre of the Spider 6 in
accordance with AC 43.13-2B, Para 105. Record the actual applied loads:
Load Case
Ultimate
Load Factor
Weight of Spider 6
Minimum Applied Load
[Load Factor x Weight]
Forward 18.0g 0.165 kg 2.970 kg
Downward 20.0g 0.165 kg 3.300 kg
Upward 5.7g 0.165 kg 0.941 kg
Side 8.0g 0.165 kg 1.320 kg